Commonwealth legislation

AD/B767/151 - In-Flight Entertainment System FAA STC SA5134NM

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Commonwealth

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legislative instrument

Plain English Summary

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Requires Boeing 767‑200 aeroplanes fitted under FAA STC SA5134NM to rewire their in‑flight entertainment (IFE) power feed from the main electrical bus to a utility bus per Flight Structures SB 90FS062-23-01 Rev 2, within 18 months; and bans installing IFE under that STC unless modified. It affects operators of those modified aircraft and matters because it ensures flight crew can remove IFE power to control smoke or fumes.

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Current sections

Direct links to the current provisions in AD/B767/151 - In-Flight Entertainment System FAA STC SA5134NM.

AD/B767/151 - In-Flight Entertainment System FAA STC SA5134NM

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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

View image in the official source

AIRWORTHINESS DIRECTIVE

View image in the official source

View image in the official source For the reasons set out in the background section, the CASA delegate whose signature appears below issues the following Airworthiness Directive (AD) under subregulation 39.1 (1) of CAR 1998. The AD requires that the action set out in the requirement section (being action that the delegate considers necessary to correct the unsafe condition) be taken in relation to the aircraft or aeronautical product mentioned in the applicability section: (a) in the circumstances mentioned in the requirement section; and (b) in accordance with the instructions set out in the requirement section; and (c) at the time mentioned in the compliance section.

Boeing 767 Series Aeroplanes

AD/B767/151 In-Flight Entertainment System FAA STC SA5134NM

10/2001

Applicability: Model 767-200 series aeroplanes modified by United States Federal Aviation Administration (FAA) Supplemental Type Certificate (STC) SA5134NM.

Requirement: 1. Modify the in-flight entertainment (IFE) system in accordance with Flight Structures Service Bulletin (SB) 90FS062-23-01, Revision 2, dated 21 September 2000 to change the source of electrical power for the IFE system from the main electrical bus to a utility electrical bus.

2. IFE may not be installed on any aeroplane in accordance with STC SA5134NM unless it is modified in accordance with Flight Structures SB 90FS062-23-01, Revision 2.

Note: FAA AD 2001-16-20 Amdt 39-12389 refers.

Compliance: For Requirement 1 - Within 18 months after the effective date of this Directive.

For Requirement 2 - As of the effective date of this Directive.

This Airworthiness Directive becomes effective on 4 October 2001.

Background: This Directive requires modification of the electrical circuits that supply power to IFE systems installed by STC SA5134NM. This action is required to ensure that, when necessary, the flight crew is able to remove power from the IFE system. Inability to remove power from the IFE system during a non-normal or emergency situation could result in inability to control smoke or fumes in the airplane flight deck or cabin.

Signature of Eugene Paul Holzapfel, Delegate of the Civil Aviation Safety Authority.

Eugene Paul Holzapfel

Delegate of the Civil Aviation Safety Authority 23 August 2001

View image in the official source

The above AD is notified in the Commonwealth of Australia Gazette on 12 September 2001.

Page 1 of 1

Source text

Sourced from the Federal Register of Legislation (legislation.gov.au), CC BY 4.0.

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?xml version="1.0" encoding="utf-8" standalone="no"?>

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

AIRWORTHINESS DIRECTIVE

For the reasons set out in the background section, the CASA delegate whose signature appears below issues the following Airworthiness Directive (AD) under subregulation 39.1 (1) of CAR 1998. The AD requires that the action set out in the requirement section (being action that the delegate considers necessary to correct the unsafe condition) be taken in relation to the aircraft or aeronautical product mentioned in the applicability section: (a) in the circumstances mentioned in the requirement section; and (b) in accordance with the instructions set out in the requirement section; and (c) at the time mentioned in the compliance section.

Boeing 767 Series Aeroplanes

AD/B767/151 In-Flight Entertainment System FAA STC SA5134NM

10/2001

Applicability: Model 767-200 series aeroplanes modified by United States Federal Aviation Administration (FAA) Supplemental Type Certificate (STC) SA5134NM.

2. IFE may not be installed on any aeroplane in accordance with STC SA5134NM unless it is modified in accordance with Flight Structures SB 90FS062-23-01, Revision 2.

Note: FAA AD 2001-16-20 Amdt 39-12389 refers.

Compliance: For Requirement 1 - Within 18 months after the effective date of this Directive.

For Requirement 2 - As of the effective date of this Directive.

This Airworthiness Directive becomes effective on 4 October 2001.